Advanced Search
Volume 40 Issue 6
Jun.  2014
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(6): 775-781.
BI Yanxian, WEI Shaoming, WANG Jun, et al. New method of scatterers association and 3D reconstruction based on multi-hypothesis tracking[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1219-1227. doi: 10.13700/j.bh.1001-5965.2015.0380(in Chinese)
Citation: Yang Jiong, Xi Ping, Hu Bifu, et al. Multi-type ribs of turbine blade modeling method fitting bowed-twist wall[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 775-781. doi: 10.13700/j.bh.1001-5965.2013.0440(in Chinese)
shu

Multi-type ribs of turbine blade modeling method fitting bowed-twist wall

doi: 10.13700/j.bh.1001-5965.2013.0440

  • School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 24 Jul 2013
  • Publish Date: 20 Jun 2014
    Abstract
  • Considering the geometric features of ribs in a bowed-twist cooling passage, a modeling method based on equidistant was presented. It generated rib tools, which was a tablet trimmed by equidistant surfaces of walls in intracavity of blade and pressure slide or suction slide, and then conducted modeling of ribbed channels. Furthermore, the principle of the modeling method was deeply analyzed, and two algorithms were developed, one recognized surfaces of walls in intracavity of blade automatically, the other matched two surfaces. The main parameters were determined as well. Meanwhile, a means based on sketch to parameterize ribbed channels was provided. Eventually, the parametric design module of ribbed channels was developed on unigraphics (UG), which achieved multiple ribbed channels modeling.

     

    • FullText(HTML)
    • References(9)
  • [1]
    航空发动机设计手册总编委会. 航空发动机手册第十册[M].北京:航空工业出版社,2000:8-9 Editorial Board of Aircraft Engine Design Manual.Aircraft engine design manual volume 10[M].Beijing:Aviation Industry Press,2000:8-9(in Chinese)
    [2]
    倪萌,朱惠人, 裘云,等.航空发动机涡轮叶片冷却技术综述[J].燃气轮机技术.2005,18(4):25-33 Ni Meng,Zhu Huiren,Qiu Yun,et al.Review of aero-turbine blade cooling technologies[J].Gas Turbine Technology,2005,18(4):25-33(in Chinese)
    [3]
    Ekkad S V, Pamula G,Shantiniketanam M.Detailed heat transfer measurements inside straight and tapered two-pass channels with rib turbulators[J].Experimental Thermal and Fluid Science,2000,22(3/4):155-163
    [4]
    夏禹. 涡轮叶片造型CAD系统研究[D].西安:西北工业大学,2004 Xia Yu.The research on turbine blade CAD modeling system[D].Xi'an:Northwestern Polytechnical University,2004(in Chinese)
    [5]
    宋田庆, 莫蓉,夏禹,等.航空发动机叶片CAD造型方法[J].航空制造技术,2007(2):78-81 Song Tianqing,Mo Rong,Xia Yu,et al.CAD modeling method for aeroengine blade[J].Aeronautical Manufacturing Technology,2007(2):78-81(in Chinese)
    [6]
    Hoschek J, Müller R.Turbine blade design by lofted B-spline surfaces[J].Journal of Computational and Applied Mathematics,2000,119(1/2):235-248
    [7]
    朱谦,宁涛, 席平.基于引导线的涡轮气冷叶片伸根建模方法[J].北京航空航天大学学报，2012,38(8):1085-1089 Zhu Qian,Ning Tao,Xi Ping.Root extending section of turbine modeling method based on guide curves[J].Journal of Beijing University of Aeronauties and Astronautics,2012,38(8): 1085-1089(in Chinese)
    [8]
    席平,朱谦, 张宝源.涡轮叶片冷气通道转接段的特征分析及建模[J].图学学报,2012,33(4):37-41 Xi Ping,Zhu Qian,Zhang Baoyuan.Feature analysis and modeling of cooling passages transition section in turbine blade[J].Journal of Graphics,2012,33(4):37-41( in Chinese)
    [9]
    Piegl L A, Tiller W.Computing offsets of NURBS curves and surfaces[J].Computer-Aided Design,1999,31(2):147-156
    • Relative Articles

  • Relative Articles

    [1]CAI S Y，HAO F W，SHI T. Partition based on features of neighborhood points and corresponding point cloud registration of aero-engine damaged blade[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：784-794 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0081.
    [2]HAN F Q，ZHANG D Y. Ultrasonic longitudinal torsional and low frequency torsional compound vibration tapping experiment[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（4）：1077-1084 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0453.
    [3]MA X，XU S，SHANG P C，et al. Fault diagnosis of gearbox under open set and cross working condition based on transfer learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1753-1760 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0719.
    [4]ZHANG Hua-bo, GUO Ying-qing, LI Gui-cai, ZHAO Wan-li, YE Peng. Modeling and parameter design methodology for component-level performance model of ducted ram air generation turbine[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0787
    [5]WANG Xiaozhe, WANG Yubo, WU Kun, WAN Zhiqiang. Structural optimization of flexible blades for vertical axis wind turbines[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0444
    [6]FU J J，XU Y，ZHOU X M，et al. Topological optimization method for conformal cellular structures on surfaces based on co-simulation[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（9）：2781-2790 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0751.
    [7]HU Jing-chen, ZHENG Guo-lei. Geometric cognitive computing method for surface iso-segmentation[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0593
    [8]WU Z C，SHAN Y，ZHANG J Z，et al. Heat transfer enhancement and ejection characteristics of mixing pipe with ribs for infrared suppressor[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：2009-2017 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0548.
    [9]LI Zhi-qiang, WANG Yang, XIN Li-biao. Structural Design and Aerodynamic Performance Analysis of Gradient Hexagonal Deformable Wing Ribs[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0669
    [10]CHEN Shi, XU He-ming, SUN Kai, XU Yi-han, ZHANG Yi-shang. Prediction of creep strain of turbine blades based on finite element nodes[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0639
    [11]TANG Y C，ZHU Q H，LIU F C，et al. Design of robust controller for single outrigger of vibration active isolation platform based on LPV[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1796-1801 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0513.
    [12]XUAN L M，ZOU Z P，ZENG F. Analyzing and modeling flow in tip clearance of transonic turbine rotor[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2374-2384 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0635.
    [13]GUO S N，SONG W，XIANG N L，et al. Dynamic characteristics of turbine flowmeter based on CFD simulation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1904-1911 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0594.
    [14]YANG W T，XU T H，WANG N Z，et al. Influence of open water in retrieval of soil moisture by spaceborne GNSS-R[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1779-1786 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0479.
    [15]HE Z P，ZHOU J X，XIN J，et al. Endwall profiling of turbine blade hub with rim seal[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2596-2607 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0728.
    [16]XU X Y，YAN G R，LEI Y. Surface quality optimization based on mutative scale chaos algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3328-3334 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0070.
    [17]ZHOU Quan-zhi, YANG You-xu, SUN Lu-bin, ZHANG Xing-cui, WU Yi-fei, HUO Meng-wen. Aeroelastic Optimization Design of SpaRibs Wing Structure[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0343
    [18]YU Yang-yi, YANG Yi-gang. Research on bi-modal imaging method for detection of residual core in hollow turbine blades[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0526
    [19]LEI J Y，LEI Q N，LI H B，et al. A mesh parameterization method and life reliability-based optimization for turbine blade[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2651-2659 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0708.
    [20]WANG Weiqi, XING Yuming, ZHENG Wenyuan, HAO Zhaolong. Phase change heat transfer characteristics and fractal optimization of radial plate fin tube[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2520-2528. doi: 10.13700/j.bh.1001-5965.2021.0140
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(1225) PDF downloads(506) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return